GE CF34-10E5A1
Service difficulty reports · 476
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'CF3410E5A1' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'CF3410E5A1' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA140728005Display · odor(CAN) AS REPORTED BY CABIN CREW. PASSENGER SEATED AT 24C COMPLAINED OF A BURNING ODOR. ELECTRICAL ODOR DETECTED FROM ROW 24AC-26AC. VIDEO SYSTEM WAS SHUTDOWN, IDENTIFIED SVDU 325A SOURCE OF ELECTRIC ODOR. CONFIRMED PREVIOUS TROUBLESHOOTING. REPLACED SEASDR CA140716012Hose · defective(CAN) FOUND NR 2 ENGINE RT BLEED SYSTEM, HPSOV SUPPLY PRESSURE SERVO LINE FOUND WITH A LEAK AT JUNCTION OF BRAIDED PART OF LINE AND ELBOW THAT CONNECTS TO THE HPSOV. ALSO NO EICAS MESSAGE AND NO CMC ACTIVE MESSAGE ON THE AIRCRAFT. THE HPSOV SUPPLY PRESSURE SSDR CA140714008Valve · failed(CAN) OPERATING UNDER MEL 36-00-00 A1 ENGINE 1 BLEED INOPERATIVE. DEPARTED WITHOUT INCIDENT. IN CLIMB THROUGH FL280 EICAS MESSAGE BLEED 2 FAIL. LEVEL OFF REQUESTED AND APPROVED AT FL280. PF CALLED FOR "CHECKLIST BLEED 2 FAIL". PM OPENED ANTIICE MFD PAGE AND ASDR CA140714010Wheel · vibration(CAN) FLIGHT SUSPECTED A BLOWN NOSE WHEEL TIRE DEPARTING. CREW REPORTED WHEEL VIBRATION FROM NOSE WHEEL. DISPATCH RECEIVED A NOTIFICATION OF A POSSIBLE INCIDENT TIRE FAIL FROM TOWER & TMU. ALL SUITABLE AUTHORITIES HAD BEEN ADVISED. FLIGHT DECLARED AN EMERGENCSDR CA140707009Actuator · failed(CAN) WHILE IN CRUISE AT FL390, ACFT LOST ENTIRE AUTO-PILOT, AND PITCH TRIM CAPABILITIES. ACFT DECLARED A "PAN PAN" WITH ATC. ACFT MAINTAINED ALTITUDE WITH FAILURE +/- 100FT. ATC BLOCKED AIRSPACE BETWEEN FL390-370. FIM TASK 27-43-00-810-801-A CARRIED OUT,SDR CA140707006Gcu · failed(CAN) AT TOP OF DESCENT THE ACFT LOST AC BUS 1 FAIL. LOST ALL DISPLAYS ON THE CAPTAIN SIDE, ALSO LOST NAV SYSTEM, SPOILERS, THRUST REVERSES AND STEERING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT ALSO LOST THE LIGHTS IN THE PASSENGER CABIN. THE CREWSDR CA140708003Fan · failed(CAN) DURING TAXI FOR DEPARTURE, FLIGHT CREW HEARD A POPPING NOISE, WHICH WAS THEN FOLLOWED BY A SMOKE ODOR IN THE COCKPIT. FLIGHT RETURNED TO THE GATE AND MTC INVESTIGATED, FOUND THE RMP PANEL WAS THE ORIGIN OF THE ISSUE. FOUND DAP NR 1 FAN FAULTED. DAP NSDR CA140714014Acm · failed(CAN) ON DEPARTURE CLIMBING THROUGH 7,000FT A BURNING ODOR WAS NOTICED THROUGH-OUT THE CABIN AND FLIGHT-DECK FOR ABOUT 5 SECONDS. ODOR WAS RECOGNIZED AGAIN AFTER TOUCH-DOWN FOR 5-10 SECONDS. IT WAS PERCEIVED AS A DOUBLE PACK FAILURE ON ARRIVAL AT THE GATE. NRSDR CA140716013Module · failed(CAN) CREW REPORTED LOSS OF PITCH CONTROL AND NO AUTO-PILOT. REPORTED A HISTORY OF THIS MAINTENANCE ISSUE WITH ACFT. HIGH SPEED LANDING AND SHORT RUNWAY LENGTH WERE FACTORS THAT DROVE THE CAPTAIN`S DECISION TO DECLARE THE PAN PAN WITH ATC. LANDING WAS CARRIEDSDR CA140627010Exhaust Duct · failed(CAN) AIR RETURN FOR DUAL BLEED FAIL, EMERGENCY DECLARED. EMERGENCY VEHICLES CALLED OUT. RESOLUTION FIM TASK 36-11-00-810-836-A CARRIED OUT. FOUND PRECOOLER EXHAUST DUCT SEAL TORN. REPLACED EXHAUST DUCT SEAL IAW AMM 36-11-08PB 401.SDR CA140630029Transceiver · failed(CAN) AFTER TAKEOFF WEATHER RADAR FAILED. ENROUTE AND DESTINATION WEATHER NOT SUITABLE FOR THE FLIGHT TO CONTINUE. ADVISED DISPATCH AND DIVERTED. WEATHER RADAR RTA REPLACED AND TESTED IAW AMM 34-42-01 PB 401, NO FAULT.SDR CA140628001Door · jammed(CAN) DURING DEPLOYMENT TEST, THE R2 DOOR JAMMED IN A PARTIALLY OPEN POSITION. IT WAS NOTED THAT THE ASSIST BOTTLE HAD FIRED, BUT THE DOOR ONLY PARTIALLY OPENED & THE SLIDE HAD NOT DEPLOYED FROM THE PACK BOARD. THE DOOR HAD BEEN IN THE ARMED POSITION, THE TESDR CA140617001Unknown · odor(CAN) DURING TAKEOFF ROLL AND INITIAL CLIMB VERY STRONG "DIRTY SOCK" ODOR NOTED BY ALL CREW. ODOR EVENTUALLY DISSIPATED BUT RETURNED ON DESCENT THROUGH 10,000 FT UNTIL LANDING. POSSIBLE CAUSE OF HYD ODOR WAS DUE TO ENGINE EDP. REPLACEMENT, L4624347. CLEANEDSDR CA140603002Module · failed(CAN) GEAR STEER FAIL CAUTION MESSAGE ON SELECTION OF GEAR DOWN FOR LANDING. USED DIFF TO STEER . RESOLUTION ACFT POWER RESET. FAULT CLEARED, NO ACTIVE FAULT, IAW FIM 45-45-00-810-973-A, TRANSITORY CONDITION OF THE STEERING MODULE, MAU2-MOD3/4. SYSTEM FUNCSDR CA140528004Acm · failed(CAN) FUMES WERE REPORTED IN CABIN BY FLIGHT CREW AND IFS- FUMES ATTRIBUTED TO A PACK FAIL. NO SMOKE WAS CITED. FLIGHT CREW DECLARED AN EMERGENCY WITH ATC UPON RETURNING. PAX REACTION WAS REPORTED GENERALLY AS GOOD. BOTH IFS AND FLIGHT CREW REPORTED FEELINGSDR CA140522002Controller · failed(CAN) SLAT FAIL MESSAGE ON THE GROUND BEFORE DEPARTURE, MESSAGE CLEARED, REOCCURRED IN THE AIR, DIVERTING. ARFF NOT CALLED. SFACE NR 1 REPLACED AND TESTED SERVICEABLE IAW AMM 27-53-02 PB 401.SDR CA140521004Slat System · failed(CAN) SLAT FAILURE IN CRUISE. MAINTENANCE ADVISED. ACCOMPLISHED FIM TASK 27-83-00-810-814-A. FAULT CLEARED PERFORMED SLAT/FLAP OPN TEST SEVERAL TIMES, CHECKS OK.SDR CA140516006Cable · sheared(CAN) R2 DISARM CABLE SHEARED. CANNOT DISARM DOOR ALTHOUGH DISARM LEVER MOVES. R2 DOOR DISARM CABLE REPLACED IAW T/C SB190-52-0042-04. OPS CHECKS CARRIED OUT OK FOR SERVICE.SDR CA140526011Rod · broken(CAN) LEFT AILERON TRIM ON TRIM IND .1250 RUDDER TRIM REQUIRED TO FLY S+L FUEL BALANCED. DURING TROUBLESHOOTING FOUND BOTH LT & RT INBD FLAP TRACKS NR 1 LOWER FLAP RODS BROKEN IN HALF. ALSO, BOTH LT AND RT INBD FLAP TRACKS NR 2 FWD RODS BENT. REF IPC 57-54-SDR CA140512008Bleed Valve · failed(CAN) RT ENGINE BLEED VALVE MEL 36-11-03 APPLIED AT DEPARTURE. BLEED WAS UNCONTROLLABLE IN-FLIGHT. FLIGHT DID AN AIRBORNE RETURN AND LANDED APPROXIMATELY 2000 LBS OVERWEIGHT. MOC ADVISED. RT NAPRSOV REPLACED IAW AMM 36-11-03-000-801-A. OPS TEST CARRIED OUTSDR CA140508004Control Lever · failed(CAN) LANDING GEAR WOULD NOT RETRACT, RETURN, LANDED AND TAXIED TO GATE WITHOUT INCIDENT. NOT AN OVERWEIGHT LANDING. L/G CONTROL LEVER LOCKED IN THE DOWN POSITION DURING TAKEOFF TROUBLESHOOTING CARRIED OUT IAW FIM 32-33-00-810-802-A, NFF. ALL POSSIBLE CAUSESDR CA140523003Line · worn(CAN) RIGHT AND LT TANK WING STUB FOUND CHAFING MARK ON FUEL LINES. THIS IS CHAFING ON THE TANK INTERNAL FUEL LINES UNDER CLAMPS FOUND DURING HEAVY MAINTENANCE.SDR CA140428002Steering Sys · malfunctioned(CAN) ON LANDING, FLIGHT EXPERIENCED EICAS MESSAGE AND LOSS OF STEERING. GROUND RESET WAS SUCCESSFUL. RESET WAS ACTIONED AND WAS SUCCESSFUL.SDR CA140425001Diffuser · cracked(CAN) FOLLOWING INSPECTION IAW MAINTENANCE PROGRAM, REFUEL ASSY DIFFUSER HAS BEEN FOUND CRACKED. RT WING FUEL TANK DIFFUSER ASSY REPLACED IAW AMM 28-23-20.SDR R61A201404190582Rub Strip · corrodedDURING HEAVY CHECK, LT ENGINE OTBD FAN COWL UPPER METALLIC STRIP WORN AND CORRODED. MX R & R LT ENGINE OTBD FAN COWL UPPER METALLIC STRIP IAW SRM 51-41-02, PN 341-2311-505, RUB STRIP.SDR R61A201404190583Rub Strip · corrodedDURING HEAVY CHECK, LT ENGINE INBD FAN COWL UPPER METALLIC STRIP WORN AND CORRODED. MAINTENANCE R & R LT ENGINE INBD FAN COWL UPPER METALLIC STRIP IAW SRM 51-41-02, PN 341-2311-505, RUB STRIP.SDR CA140414005Blade · lack of lube(CAN) AFTER DEPARTURE, THE CREW NOTICED EXCESSIVE ENGINE VIBRATION. AFTER CONSULTATION WITH MAINTENANCE, IT WAS DECIDED THAT THE FLIGHT SHOULD RETURN. CARRIED OUT NR 1 ENGINE BLADE LUBE IAW EMM 72-00-00-030-806, 72-00-00-030-808 & 72-00-00-030-805, PERFORMED SDR CA140404004Warning Message · activated(CAN) ON APPROACH, CREW HAD THREE FAULTS, ASSOC SPOILERS/AVIONICS MAN3B. A PATCH WAS DONE WITH MOC AND SPOILERS WERE DEEMED INOPERATIVE. CREW DECLARED A PAN PAN WITH ATC AND EMERGENCY SERVICES WERE CALLED OUT. FLIGHT LANDED ON RWY AND TAXIED TO GATE WITH NOSDR CA140331002Slat System · malfunctioned(CAN) ARRIVED WITH A SLAT PROBLEM. REPLACED SERVICEABLE LT OTBD SLAT SKEW SENSOR 2 & 3 IAW AMM 27-83-01PB401.SDR CA140321014Sensor · failed(CAN) AS A RESULT OF NUMEROUS INDICATIONS, MOSTLY CONCERNING A FLAP FAILURE, THE CREW DECLARED AN EMER, RESULTING IN THE EMER VEHICLES MEETING THE FLIGHT ON ARRIVAL. DUTY PILOT, FLIGHT SAFETY & MTC CONTROL ADVISED. CHANGED LT FLAP POSITION SENSOR IAW AMM 27-SDR CA140514005Feel Unit · interference(CAN) INTERFERENCE WAS FOUND BETWEEN LT WHEEL WELL STRUCTURE, FR52 AND AILERON FEEL UNIT WHEN FULLY TRIM RT WING DOWN. INTERFERENCE BETWEEN STRUCTURE & AILERON FEEL UNIT PERMANENTLY REPAIRED IAW ETD 2014-190-023347 & ERJ190-53-53144. HFEC C/O AT BLENDED AREASDR CA140310003Warning Message · activated(CAN) ACFT HAD AN EICAS STEERING FAIL MESSAGE ON RUNWAY PRIOR TO TAKEOFF. CREW PERFORMED SUCCESSFUL RESET. INBOUND FLIGHTS HAD TO ABORT LANDING WHILE RESET BEING COMPLETED. FLIGHT THEN DEPARTED WITHOUT INCIDENT.SDR CA140310001Lanyard · broken(CAN) R2 DOOR ESCAPE SLIDE FOUND WITH LACING BROKEN.SDR CA140514008Torque Tube · grooved(CAN) FOUND RT WING FLAP TORQUE TUBE F6 DAMAGED. GROOVED BY ADJACENT GUARD BRACKET. IT APPEARS THAT THE T TUBE CAME IN CONTACT WITH THE GUARD & DAMAGED BOTH PARTS.SDR CA140304002Brake Assy · seized(CAN) AIRCRAFT ARRIVED AT GATE WITH THE NR 1 BRAKE SEIZED, CAUSED THE NR 1 TIRE TO BLOW AT THE GATE WITH PASSENGERS AND CREW ON THE ACFT. NR 1 & 2 MAIN WHEEL ASSY REPLACED IAW TASK CARDS E19-32-49-05-400-801-A & E19-32-49-05-000-801-A. NR 1 MAIN WHEEL BREAKSDR CA140225018Actuator · faulted(CAN) AFTER LANDING, ENGINE 1 REV FAIL. ENG 1 REV PROT FAULT. ENG 1, NO DISPATCH. FOUND OTBD UPPER T/R ACTUATOR ROD END CAP LOOSE AND LEAKING. FOUND NR 1 REVERSER UPPER LT FEEDBACK ACTUATOR, LEAKING ACTUATOR REPLACED IAW AMM 78-30-05-PB301. 78-32-03-400-8SDR CA140225004Fadec · malfunctioned(CAN) ENROUTE, FLIGHT NOTIFIED MAINTENANCE CONTROL THAT THE LT ENGINE HAD ROLLED BACK TWICE FOLLOWED BY EICAS MESSAGE "ENG 1 TLA FAIL" ALONG WITH "ELEV THR COMP FAIL". THE ENGINE STABALIZED AFTER THE AUTO THRUST SYS WAS TURNED OFF AND THE FLIGHT CONTINUED. IASDR CA140225003Engine · vibration(CAN) IMMEDIATELY AFTER DEPARTURE DURING CLIMB, THE ACFT EXPERIENCED ENGINE VIBRATIONS FROM THE NR 1 ENGINE. THE FLIGHT LEVELED OFF AT 13,000 FT AND THE VIBRATIONS SUBSIDED. THE CREW RECOMMENCED THE CLIMB TO 17,000 FT WITH THE VIBRATION RETURNING. THE CREW ESDR CA140410001Line · chafed(CAN) DURING FLAP ACTUATOR 2L INSTALLATION, IT WAS FOUND THAT THE EDP SUCTION LINE WAS CHAFING ON THE FIRE EXTINGUISHER TUBING ON THE LT WING INBD AFT SPAR. THE DAMAGE ON THE FIRE EXTINGISHER TUBE IS OUT OF LIMITS IAW AMM 20-10-03, TABLE 802. EDP SUCTION LINSDR CA140205004Torque Tube · misinstalled(CAN) DURING FINAL AVIONOCS INSPECTION, FOUND FLAP TORQUE TUBE F2 IN THE MID EBAY NOT INSTALLED CORRECTLY, BOLT NOT THROUGH HOLE IN TUBE. AFTER PULLING ON TUBES, IT DETACHED FROM GEARBOX.SDR CA140130001Starter Gen · cracked(CAN) AFTER RUN-UP, FOUND MAJOR LEAK IN APU COMPARTMENT. AFTER INVESTIGATION FOUND APU GENERATOR CRACKED.SDR CA140129002Slat System · failed(CAN) ON APPROACH, ACFT HAD A SLAT FAIL, CREW DID A MISSED APPROACH AND DID AN IN AIR RESET THAT WAS SUCCESSFUL. FLIGHT LANDED ON SECOND ON 2ND ATTEMPT WITHOUT FURTHER INCIDENT. NO PAX REACTION. QRH PROCEDURE ACCOMPLISHED, MSG CLEARED. ASSOCIATED MSG ARE ASDR CA140124016Wire Harness · failed(CAN) AFTER TAKEOFF THE CREW WAS UNABLE TO MOVE THE LANDING GEAR LEVER INTO THE "UP" POSITION. THEY ELECTED TO RETURN, MAINTENANCE IS INVESTIGATING. RESOLUTION: RT MLG WOW SENSOR 2 REPLACED IAW AMM 32-62-03-000/400-801A. RT MLG SENSOR 2 HARNESS REPLACED IAW SDR CA140124018Processor · failed(CAN) WHILE IN CRUISE, AN AVIONICS MAU 1 FAILURE OCCURRED. THE CREW DECLARED A PAN PAN AND DIVERTED. APPROACH AND LANDING CARRIED OUT WITHOUT INCIDENT. EMERGENCY VEHICLES WERE CALLED OUT. CONNECTED THE CAPTAIN WITH THE DUTY PILOT SO THEY COULD DISCUSS THE SDR CA140122005Control Unit · failed(CAN) FLIGHT HAD A SLAT FAIL, NO EMERGENCY DECLARED AND ACFT LANDED WITHOUT FURTHER INCIDENT REPLACED NR 1 SFACE IAW AMM 27-53-02, OPS TEST COMPLETED IAW 27-80-00-710-801-A AND 27-50-00-710-801-A. ACFT OK FOR SERVICE.SDR CA140121001Sensor · failed(CAN) AT APPROXIMATELY 6000 FT DESCENDING THE CREW NOTICED A FLAP/SLAT FAILURE MESSAGE. THEY DECLARED A PAN MSG WITH ATC AND LANDED WITHOUT INCIDENT. REPLACED RT WING OTBD SKEW SENSORS S2/S3 AND S3/S4 IAW AMM 27-83-01/401 RT WING SLAT DRIVE TORQUE TUBE S2 REMSDR CA140203015Mount · chafed(CAN) ACCOMPLISHING A B3 MAINTENANCE CHECK. NR 1 ENGINE AFT MOUNT FITTING CHAFED ON INBD CLEVIS AFT LUG FWD UPPER FACE.SDR CA140117008Baffle · cracked(CAN) BAFFLE INSIDE RT WING REFUELLING DIFFUSER IS CRACKED. RT WING REFUELLING DIFFUSER REPLACED IAW AMM 28-23-20, PB401.SDR CA140103014Aileron Sys · stiff(CAN) DURING DESCENT, CREW DISCONNECTED THE AUTOPILOT, AT WHICH TIME THEY NOTICED THE AILERON AND ROLL CONTROL WERE VERY STIFF, CREW STATED THAT THE ACFT REMAINED LEVEL BUT VERY DIFFICULT. EXCESSIVE CLEAN OFF AILERON ARTIFICAL FEEL UNIT INPUT SHAFT-LT WHEEL WSDR CA140103015Pitot Tube · failed(CAN) CREW HAD ADS 2 HEATER FAIL, ADS 3 SLIP COMP FAIL AND ADS 4 SLIP COMP FAIL F/O WAS PILOT FLYING, THE CHECKLIST SAID TO REVERT TO ADS 3 MANUALLY, F/O`S SIDE SHOWED V/S OF 500FT IAW MIN AND ALTITUDE +/- 50FT WHICH CREW COULD FEEL. CAPT`S SIDE REMAINED NORMA
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